FR2173143A1 - - Google Patents
Info
- Publication number
- FR2173143A1 FR2173143A1 FR7306172A FR7306172A FR2173143A1 FR 2173143 A1 FR2173143 A1 FR 2173143A1 FR 7306172 A FR7306172 A FR 7306172A FR 7306172 A FR7306172 A FR 7306172A FR 2173143 A1 FR2173143 A1 FR 2173143A1
- Authority
- FR
- France
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Granted
Links
Classifications
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02C—GAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
- F02C6/00—Plural gas-turbine plants; Combinations of gas-turbine plants with other apparatus; Adaptations of gas-turbine plants for special use
- F02C6/20—Adaptations of gas-turbine plants for driving vehicles
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02C—GAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
- F02C7/00—Features, components parts, details or accessories, not provided for in, or of interest apart form groups F02C1/00 - F02C6/00; Air intakes for jet-propulsion plants
- F02C7/36—Power transmission arrangements between the different shafts of the gas turbine plant, or between the gas-turbine plant and the power user
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02C—GAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
- F02C9/00—Controlling gas-turbine plants; Controlling fuel supply in air- breathing jet-propulsion plants
- F02C9/16—Control of working fluid flow
- F02C9/20—Control of working fluid flow by throttling; by adjusting vanes
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Physics & Mathematics (AREA)
- Fluid Mechanics (AREA)
- Control Of Eletrric Generators (AREA)
- Control Of Velocity Or Acceleration (AREA)
- Feedback Control In General (AREA)
- Supercharger (AREA)
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
DE2208040A DE2208040C3 (de) | 1972-02-21 | 1972-02-21 | Regelschaltung für die Prozeßtemperatur einer Gasturbine |
Publications (2)
Publication Number | Publication Date |
---|---|
FR2173143A1 true FR2173143A1 (nl) | 1973-10-05 |
FR2173143B3 FR2173143B3 (nl) | 1976-02-20 |
Family
ID=5836587
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
FR7306172A Expired FR2173143B3 (nl) | 1972-02-21 | 1973-02-21 |
Country Status (8)
Country | Link |
---|---|
US (1) | US3844114A (nl) |
JP (1) | JPS5532893B2 (nl) |
CH (1) | CH552132A (nl) |
DE (1) | DE2208040C3 (nl) |
FR (1) | FR2173143B3 (nl) |
GB (1) | GB1424138A (nl) |
IT (1) | IT973278B (nl) |
SE (1) | SE384901B (nl) |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
EP0471623A1 (fr) * | 1990-08-16 | 1992-02-19 | Societe Nationale D'etude Et De Construction De Moteurs D'aviation "Snecma" | Dispositif compensateur de température devant la turbine d'une turbomachine d'aviation |
Families Citing this family (16)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE2241363B2 (de) * | 1972-08-23 | 1975-01-09 | Motoren- Und Turbinen-Union Muenchen Gmbh, 8000 Muenchen | Regeleinrichtung für ein Gasturbinentriebwerk, insbesondere eines Kraftfahrzeugs |
US3938321A (en) * | 1974-03-04 | 1976-02-17 | General Motors Corporation | Gas turbine control |
US3952502A (en) * | 1974-03-04 | 1976-04-27 | General Motors Corporation | Gas turbine control |
US4134258A (en) * | 1974-06-10 | 1979-01-16 | Nippondenso Co., Ltd. | Fuel control system |
GB1520412A (en) * | 1974-07-09 | 1978-08-09 | Lucas Industries Ltd | Gas turbine engine fuel control systems |
US4016717A (en) * | 1975-02-19 | 1977-04-12 | Westinghouse Electric Corporation | Matching response of a blade path temperature limit signal to characteristics of a gas turbine |
JPS598653B2 (ja) * | 1975-10-11 | 1984-02-25 | 三菱重工業株式会社 | ジドウシヤヨウ 2 ジクガスタ−ビンノセイギヨソウチ |
US4206597A (en) * | 1976-04-23 | 1980-06-10 | The Boeing Company | Fan R.P.M. control loop stabilization using high rotor speed |
US4314441A (en) * | 1977-07-22 | 1982-02-09 | Westinghouse Electric Corp. | Gas turbine power plant control apparatus including an ambient temperature responsive control system |
US4197699A (en) * | 1977-12-22 | 1980-04-15 | The Garrett Corporation | Free turbine type gas turbine engine with variable free turbine guide vane control system |
US4543782A (en) * | 1982-05-21 | 1985-10-01 | Lucas Industries | Gas turbine engine fuel control systems |
JPS5910742A (ja) * | 1982-07-08 | 1984-01-20 | Toyota Motor Corp | ガスタ−ビン機関の制御装置 |
JP2743516B2 (ja) * | 1989-10-05 | 1998-04-22 | トヨタ自動車株式会社 | 二軸式ガスタービン機関 |
US5379584A (en) * | 1992-08-18 | 1995-01-10 | Alliedsignal Inc. | Synthesis of critical temperature of a turbine engine |
JP5725817B2 (ja) * | 2010-11-30 | 2015-05-27 | 三菱日立パワーシステムズ株式会社 | ガスタービン制御装置および発電システム |
CN102890517B (zh) * | 2011-07-20 | 2015-01-07 | 烟台杰瑞石油装备技术有限公司 | 一种直燃式液氮蒸发器的控制设备 |
Family Cites Families (7)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB1090143A (en) * | 1965-04-07 | 1967-11-08 | Hawker Siddeley Dynamics Ltd | Improvements in or relating to electrical control systems for engines |
GB1215931A (en) * | 1967-03-11 | 1970-12-16 | Rolls Royce | Improvements in or relating to gas turbine engines |
GB1205323A (en) * | 1968-01-22 | 1970-09-16 | Mini Of Technology | Engine fuel supply servo systems |
US3470691A (en) * | 1968-06-17 | 1969-10-07 | Avco Corp | Automatic starting and protection system for a gas turbine |
US3606754A (en) * | 1969-05-19 | 1971-09-21 | Chandler Evans Inc | Hybrid fuel control |
US3601984A (en) * | 1969-10-27 | 1971-08-31 | Gen Electric | Temperature rate control system |
US3780527A (en) * | 1971-04-21 | 1973-12-25 | Lucas Industries Ltd | Control apparatus for a gas turbine engine |
-
1972
- 1972-02-21 DE DE2208040A patent/DE2208040C3/de not_active Expired
- 1972-12-29 IT IT34077/72A patent/IT973278B/it active
-
1973
- 1973-01-29 CH CH122573A patent/CH552132A/xx not_active IP Right Cessation
- 1973-02-01 US US00328710A patent/US3844114A/en not_active Expired - Lifetime
- 1973-02-19 GB GB800773A patent/GB1424138A/en not_active Expired
- 1973-02-20 JP JP2060973A patent/JPS5532893B2/ja not_active Expired
- 1973-02-20 SE SE7302346A patent/SE384901B/xx unknown
- 1973-02-21 FR FR7306172A patent/FR2173143B3/fr not_active Expired
Cited By (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
EP0471623A1 (fr) * | 1990-08-16 | 1992-02-19 | Societe Nationale D'etude Et De Construction De Moteurs D'aviation "Snecma" | Dispositif compensateur de température devant la turbine d'une turbomachine d'aviation |
FR2665927A1 (fr) * | 1990-08-16 | 1992-02-21 | Snecma | Dispositif compensateur de temperature devant la turbine d'une turbomachine d'aviation. |
US5157918A (en) * | 1990-08-16 | 1992-10-27 | Societe Nationale D'etude Et De Construction De Motors D'aviation | Temperature compensating device for turboshaft aero-engines |
Also Published As
Publication number | Publication date |
---|---|
DE2208040C3 (de) | 1979-05-23 |
JPS4896909A (nl) | 1973-12-11 |
US3844114A (en) | 1974-10-29 |
IT973278B (it) | 1974-06-10 |
DE2208040B2 (de) | 1978-10-05 |
JPS5532893B2 (nl) | 1980-08-27 |
FR2173143B3 (nl) | 1976-02-20 |
DE2208040A1 (de) | 1973-09-06 |
CH552132A (de) | 1974-07-31 |
SE384901B (sv) | 1976-05-24 |
GB1424138A (en) | 1976-02-11 |